CFR 14-25.307-2014
Aeronautics and space. Part25:Airworthiness standards: transport category airplanes. SubpartC:Structure. Section25.307:Proof of structure.

Standard No.

CFR 14-25.307-2014

Release Date

2014

Published By

US-CFR-file

Latest

CFR 14-25.307-2014

Scope

(a) Compliance with the strength and deformation requirements of this subpart must be shown for each critical loading condition. Structural analysis may be used only if the structure conforms to that for which experience has shown this method to be reliable. In other cases, substantiating tests must be made to load levels that are sufficient to verify structural behavior up to loads specified in § 25.305.

CFR 14-25.307-2014 history

• 2014 CFR 14-25.307-2014 Aeronautics and space. Part25:Airworthiness standards: transport category airplanes. SubpartC:Structure. Section25.307:Proof of structure.